<p>A compressor for a gas turbine engine has a split case (4) and a split stator vane inner shroud (36). Selected rotatable stator vanes (16) longitudinally restrain the shroud (36) and seal (38) carried thereon to retain the desired roundness.</p>
申请公布号
DE3874439(D1)
申请公布日期
1992.10.15
申请号
DE19883874439
申请日期
1988.07.07
申请人
UNITED TECHNOLOGIES CORP., HARTFORD, CONN., US
发明人
DITTBERNER, JR., RICHARD H., OLD SAYBROOK CONNECTICUT 06475, US;FRESCHLIN, HARRY G., MANCHESTER CONNECTICUT 06040, US;KURTI, ALEX, WEST HARTFORD CONNECTICUT 06117, US
